US6725876B2 - Control valve with integrated electro-hydraulic actuator - Google Patents

Control valve with integrated electro-hydraulic actuator Download PDF

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Publication number
US6725876B2
US6725876B2 US09/977,566 US97756601A US6725876B2 US 6725876 B2 US6725876 B2 US 6725876B2 US 97756601 A US97756601 A US 97756601A US 6725876 B2 US6725876 B2 US 6725876B2
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Prior art keywords
hydraulic
valve
fuel
control valve
fuel control
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US09/977,566
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US20030070711A1 (en
Inventor
Gary M. Bowman
Wade A. Burdick
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Woodward Inc
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Woodward Governor Co
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Priority to US09/977,566 priority Critical patent/US6725876B2/en
Assigned to WOODWARD GOVERNOR COMPANY reassignment WOODWARD GOVERNOR COMPANY ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: BOWMAN, GARY M., BURDICK, WADE A.
Priority to AU2002357658A priority patent/AU2002357658A1/en
Priority to PCT/US2002/032860 priority patent/WO2003033889A2/en
Priority to DE10297340T priority patent/DE10297340B4/en
Priority to JP2003536596A priority patent/JP4272062B2/en
Publication of US20030070711A1 publication Critical patent/US20030070711A1/en
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M21/00Apparatus for supplying engines with non-liquid fuels, e.g. gaseous fuels stored in liquid form
    • F02M21/02Apparatus for supplying engines with non-liquid fuels, e.g. gaseous fuels stored in liquid form for gaseous fuels
    • F02M21/0218Details on the gaseous fuel supply system, e.g. tanks, valves, pipes, pumps, rails, injectors or mixers
    • F02M21/023Valves; Pressure or flow regulators in the fuel supply or return system
    • F02M21/0233Details of actuators therefor
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/22Fuel supply systems
    • F02C7/232Fuel valves; Draining valves or systems
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C9/00Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F02C9/26Control of fuel supply
    • F02C9/263Control of fuel supply by means of fuel metering valves
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02MSUPPLYING COMBUSTION ENGINES IN GENERAL WITH COMBUSTIBLE MIXTURES OR CONSTITUENTS THEREOF
    • F02M21/00Apparatus for supplying engines with non-liquid fuels, e.g. gaseous fuels stored in liquid form
    • F02M21/02Apparatus for supplying engines with non-liquid fuels, e.g. gaseous fuels stored in liquid form for gaseous fuels
    • F02M21/0218Details on the gaseous fuel supply system, e.g. tanks, valves, pipes, pumps, rails, injectors or mixers
    • F02M21/023Valves; Pressure or flow regulators in the fuel supply or return system
    • F02M21/0239Pressure or flow regulators therefor
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T10/00Road transport of goods or passengers
    • Y02T10/10Internal combustion engine [ICE] based vehicles
    • Y02T10/30Use of alternative fuels, e.g. biofuels
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S277/00Seal for a joint or juncture
    • Y10S277/928Seal including pressure relief or vent feature
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10STECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10S277/00Seal for a joint or juncture
    • Y10S277/93Seal including heating or cooling feature
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T137/00Fluid handling
    • Y10T137/5762With leakage or drip collecting
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T137/00Fluid handling
    • Y10T137/6416With heating or cooling of the system
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T137/00Fluid handling
    • Y10T137/7722Line condition change responsive valves
    • Y10T137/7758Pilot or servo controlled
    • Y10T137/7759Responsive to change in rate of fluid flow
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T137/00Fluid handling
    • Y10T137/7722Line condition change responsive valves
    • Y10T137/7758Pilot or servo controlled
    • Y10T137/7761Electrically actuated valve

Definitions

  • the present invention relates generally to valves, and more particularly relates to hydraulically actuated control valves.
  • Process control valves are used in many industrial settings for a variety of applications.
  • One application is the control of gas fuel flow to the combustion system of an industrial (or utility) gas turbine wherein the valves used typically require highly linear critical gas flow versus stroke relationship.
  • Typical embodiments of the process control valves used for gas fuel flow control consist of bonnet style valves with a protruding shaft connected to an industrial hydraulic actuator.
  • Typical designs use industrial standard hardware with a self-contained process valve coupled to a hydraulic cylinder. These designs have two problems. The first problem is that the designs have long lengths of unsupported control surfaces and are massive in terms of size and weight. As a result, the design is susceptible to vibration induced failures. The second problem is that feedback devices, which are used for position control of the valve position, are coupled outside the centerline of the valve/actuator assembly at the end opposite the valve. The long lengths in combination with the temperature differentials from the end to end of the actuator assembly and the off centerline location of the feedback devices leads to degradation of the accuracy of the feedback over all operating conditions.
  • the invention provides a compact fuel control valve where a hydraulic manifold is used as both a valve bonnet and an actuator seat for the valve actuator. This reduces the number of parts required to maintain functionality while providing adequate structural support of the fuel control valve.
  • the valve body has a fuel inlet, a fuel outlet and a valve metering plug opening.
  • a metering plug guide is mounted within the valve metering plug opening and is attached to the hydraulic manifold, and it forms a thermal barrier between the valve body and the hydraulic manifold to protect lower temperature components from high temperature gaseous fluids.
  • the metering plug guide has an aperture that accepts a valve metering plug that is directly coupled to the actuator piston.
  • the coupling is made within the hydraulic fluid, which provides hydraulic damping of vibrations induced into the coupling.
  • the hydraulic manifold maintains barriers between the hydraulics and the gaseous fuel. Dual redundant hydraulic seals are between the actuation area and a hydraulic seal leakage path along the metering plug to reduce leakage of hydraulic fluid from the actuation area during operation. Dual redundant gas seals to reduce fuel leakage from the valve body are placed between the valve body and a gas seal leakage path along the metering plug.
  • the hydraulic seal leakage path within the hydraulic manifold is routed into a hydraulic drain connection and the gas seal leakage path is routed to a vent system. An intermediate vent within the hydraulic manifold that is routed to atmosphere further maintains physical separation of the gas and hydraulic system.
  • FIG. 1 is a perspective view of a fuel control valve in accordance with the present invention
  • FIG. 2 is a cross-sectional view of one embodiment of the fuel control valve of FIG. 1;
  • FIG. 3 is a cross-sectional view of another embodiment of the fuel control valve of FIG. 1;
  • FIG. 4 is an enlarged cross-sectional view of the fluid to fluid barriers of the fuel control valve of FIG. 1
  • the present invention provides a compact packaged fuel control valve that controls the flow of fuel for an industrial or utility gas turbine or other continuous combustion system.
  • a fuel control valve 20 is illustrated in FIG. 1 .
  • the fuel control valve 20 is a valve that integrates an electro-hydraulic actuator with fluid to fluid isolation barriers into a compact design.
  • the valve body 22 has a fuel inlet 24 , a fuel outlet 26 and a valve metering plug opening 28 for a valve metering plug guide 30 .
  • a hydraulic manifold 32 is mounted on the valve metering plug guide 30 and is retained to the valve body 22 by manifold bolts 34 .
  • the valve metering plug guide 30 provides a low profile thermal barrier to protect lower temperature components from the high temperature gaseous fuels flowing through the valve body 22 .
  • the hydraulic manifold 32 is used as a valve bonnet for the valve body 22 and has a valve seat 36 for receiving a stepped end 38 of the actuator 40 .
  • the actuator 40 has an actuator cylinder 42 contains an actuator piston 44 that has an actuation area 46 .
  • Hydraulic seals 48 provide a dynamic seal between the actuator piston 44 and atmosphere.
  • Piston bearing 50 supports the actuator piston's alignment within the actuator cylinder 42 .
  • the actuator piston 44 has a threaded aperture 54 for receiving a valve metering plug 56 .
  • the valve metering plug 56 has a threaded aperture and the actuator piston is threaded into the aperture.
  • the actuator 40 is a single acting spring-loaded design for fail-safe operation.
  • the springs 52 are located within the actuator cylinder 42 and are sized to provide sufficient closing force to move the actuator piston 44 to a closed position in the event of a failure.
  • the springs 52 are held in place by the stepped end 53 a of the actuator piston 44 .
  • the springs 52 may be held in place by a separate stepped piece 53 b (see FIG. 3 ).
  • a position feedback device 58 is located within the actuator cylinder 42 and is coupled to the actuator piston 44 on the centerline of the actuator 40 within the inner diameter of the springs 52 .
  • the position feedback device 58 provides actuator piston position information to a control system (not shown).
  • the centerline coupling reduces the affects of thermal expansion on accuracy and repeatability of the position feedback device 58 over all operating conditions.
  • the position feedback device 58 is an LVDT.
  • the LVDT is a dual coil, dual rod device (i.e., a duplex device).
  • the LVDT may be a simplex device.
  • the position feedback device 58 may be directly coupled to the actuator piston 44 or may be mounted on bearings that isolate the position feedback device 58 .
  • the valve metering plug 56 is mounted within an aperture 60 of the valve metering plug guide 30 .
  • the valve metering plug 56 has a contoured surface 62 that is shaped to provide linear gas flow versus actuator piston stroke (i.e., position) at constant upstream pressure.
  • the fuel control valve 20 includes a hydraulic filter 64 for last chance filtration of fluid to ensure long lasting operation of the actuator and servo valve 66 .
  • the servo valve 66 directs hydraulic fluid to appropriate cavities with the hydraulic manifold 32 to position the actuator piston 44 .
  • the servo valve 66 may be simplex, redundant, or a triple coil design.
  • the valve metering plug guide 30 and hydraulic manifold 32 contain several provisions (i.e. barriers) to maintain fluid to fluid isolation. These barriers protect the hydraulic systems from ingress of high pressure, high temperature gaseous fuels and the gas fuel system from potential ingress from the hydraulic pressure. As previously indicated, the valve metering plug guide 30 acts as a thermal barrier between the valve body 22 and the hydraulic manifold 32 . Turning now to FIG. 4, the barriers are provided in a small envelope and consist of leakage paths, vents, and seals. The gas fuel system is protected from the hydraulic system by a pair of hydraulic seals 68 that form a dual redundant seal that reduces leakage of hydraulic fluid from the actuation area 46 .
  • hydraulic drain connection 70 is shown as being near the fuel inlet for purposes of illustration. Those skilled in the art will recognize that the drain connection 70 may be located anywhere along the hydraulic manifold 32 . Hydraulic seal 74 is used to prevent hydraulic fluid from seeping into the gas fuel system. Any hydraulic fluid that seeps past hydraulic seal 74 is vented into the atmosphere via intermediate vent 76 .
  • the hydraulic system is protected from the gas fuel system by a pair of gas seals 78 that form a dual redundant seal that reduces leakage of gaseous fuel from the valve body 22 .
  • Any fuel that escapes through the gas seals 78 is routed into a customer vent system via a gas seal leakage path 80 .
  • Gas seal 82 is used to prevent gaseous fuel from ingress into the hydraulic system. Any gaseous fuel that flows past gas seal 82 is vented into the atmosphere via intermediate vent 76 .
  • an external controller commands the servo valve 66 to modulate the position of the actuator piston 44 by directing fluid into or out of the actuation area 46 via paths in the hydraulic manifold 32 to move the actuator piston 44 up or down, thereby moving the valve metering plug 56 to the position required for the desired gaseous fuel flow rate.
  • the output signal of the position feedback device 58 is sent to the external controller for use in the controller's position control loop.
  • a compact gas fuel control valve has been described.
  • the overall size and weight is approximately fifty percent less than standard commercial valves due to the integration of the actuator 40 , hydraulic manifold 32 and valve body 22 into a compact package.
  • the package increases the natural frequency of the control valve 20 to levels that are well above the frequencies that industrial or utility gas turbines operate, which in turn, substantially reduces the susceptibility of failure due to vibration.
  • the elimination of a separate valve bonnet and actuator cylinder cap reduces the number of components in the gas fuel control valve. The reduction of components increases reliability of the system and reduces the cost of the system while maintaining equivalent or greater functionality.

Abstract

A compact fuel control valve is presented where a hydraulic manifold is used as both a valve bonnet and an actuator seat for the valve actuator. The valve body has a fuel inlet, a fuel outlet and a metering plug opening. A metering plug guide mounted within the metering plug opening and attached to the hydraulic manifold forms a thermal barrier between the valve body and the hydraulic manifold to protect lower temperature components from high temperature gaseous fluids. A valve metering plug is directly coupled to the valve actuator piston. The hydraulic manifold maintains barriers between the hydraulics and the gaseous fuel with redundant seals and leakage paths. An intermediate vent within the hydraulic manifold routed to atmosphere further maintains physical separation of the gas and hydraulic system.

Description

FIELD OF THE INVENTION
The present invention relates generally to valves, and more particularly relates to hydraulically actuated control valves.
BACKGROUND OF THE INVENTION
Process control valves are used in many industrial settings for a variety of applications. One application is the control of gas fuel flow to the combustion system of an industrial (or utility) gas turbine wherein the valves used typically require highly linear critical gas flow versus stroke relationship. Typical embodiments of the process control valves used for gas fuel flow control consist of bonnet style valves with a protruding shaft connected to an industrial hydraulic actuator.
Typical designs use industrial standard hardware with a self-contained process valve coupled to a hydraulic cylinder. These designs have two problems. The first problem is that the designs have long lengths of unsupported control surfaces and are massive in terms of size and weight. As a result, the design is susceptible to vibration induced failures. The second problem is that feedback devices, which are used for position control of the valve position, are coupled outside the centerline of the valve/actuator assembly at the end opposite the valve. The long lengths in combination with the temperature differentials from the end to end of the actuator assembly and the off centerline location of the feedback devices leads to degradation of the accuracy of the feedback over all operating conditions.
BRIEF SUMMARY OF THE INVENTION
The invention provides a compact fuel control valve where a hydraulic manifold is used as both a valve bonnet and an actuator seat for the valve actuator. This reduces the number of parts required to maintain functionality while providing adequate structural support of the fuel control valve. The valve body has a fuel inlet, a fuel outlet and a valve metering plug opening. A metering plug guide is mounted within the valve metering plug opening and is attached to the hydraulic manifold, and it forms a thermal barrier between the valve body and the hydraulic manifold to protect lower temperature components from high temperature gaseous fluids. The metering plug guide has an aperture that accepts a valve metering plug that is directly coupled to the actuator piston. The coupling is made within the hydraulic fluid, which provides hydraulic damping of vibrations induced into the coupling.
The hydraulic manifold maintains barriers between the hydraulics and the gaseous fuel. Dual redundant hydraulic seals are between the actuation area and a hydraulic seal leakage path along the metering plug to reduce leakage of hydraulic fluid from the actuation area during operation. Dual redundant gas seals to reduce fuel leakage from the valve body are placed between the valve body and a gas seal leakage path along the metering plug. The hydraulic seal leakage path within the hydraulic manifold is routed into a hydraulic drain connection and the gas seal leakage path is routed to a vent system. An intermediate vent within the hydraulic manifold that is routed to atmosphere further maintains physical separation of the gas and hydraulic system.
These and other advantages of the invention, as well as additional inventive features, will be apparent from the description of the invention provided herein.
BRIEF DESCRIPTION OF THE DRAWINGS
The accompanying drawings incorporated in and forming a part of the specification illustrate several aspects of the present invention, and together with the description serve to explain the principles of the invention. In the drawings:
FIG. 1 is a perspective view of a fuel control valve in accordance with the present invention;
FIG. 2 is a cross-sectional view of one embodiment of the fuel control valve of FIG. 1;
FIG. 3 is a cross-sectional view of another embodiment of the fuel control valve of FIG. 1; and
FIG. 4 is an enlarged cross-sectional view of the fluid to fluid barriers of the fuel control valve of FIG. 1
While the invention will be described in connection with certain preferred embodiments, there is no intent to limit it to those embodiments. On the contrary, the intent is to cover all alternatives, modifications and equivalents as included within the spirit and scope of the invention as defined by the appended claims.
DETAILED DESCRIPTION OF THE INVENTION
The present invention provides a compact packaged fuel control valve that controls the flow of fuel for an industrial or utility gas turbine or other continuous combustion system. Turning to the drawings, wherein like reference numerals refer to like elements, an exemplary embodiment of a fuel control valve 20 according to the present invention is illustrated in FIG. 1. As will be appreciated from the following description, the fuel control valve 20 is a valve that integrates an electro-hydraulic actuator with fluid to fluid isolation barriers into a compact design.
Turning now to FIGS. 1 to 3, the valve body 22 has a fuel inlet 24, a fuel outlet 26 and a valve metering plug opening 28 for a valve metering plug guide 30. A hydraulic manifold 32 is mounted on the valve metering plug guide 30 and is retained to the valve body 22 by manifold bolts 34. The valve metering plug guide 30 provides a low profile thermal barrier to protect lower temperature components from the high temperature gaseous fuels flowing through the valve body 22. The hydraulic manifold 32 is used as a valve bonnet for the valve body 22 and has a valve seat 36 for receiving a stepped end 38 of the actuator 40.
The actuator 40 has an actuator cylinder 42 contains an actuator piston 44 that has an actuation area 46. Hydraulic seals 48 provide a dynamic seal between the actuator piston 44 and atmosphere. Piston bearing 50 supports the actuator piston's alignment within the actuator cylinder 42. In one embodiment, the actuator piston 44 has a threaded aperture 54 for receiving a valve metering plug 56. Alternatively, the valve metering plug 56 has a threaded aperture and the actuator piston is threaded into the aperture. The actuator 40 is a single acting spring-loaded design for fail-safe operation. The springs 52 are located within the actuator cylinder 42 and are sized to provide sufficient closing force to move the actuator piston 44 to a closed position in the event of a failure. The springs 52 are held in place by the stepped end 53 a of the actuator piston 44. Alternatively, the springs 52 may be held in place by a separate stepped piece 53 b (see FIG. 3).
A position feedback device 58 is located within the actuator cylinder 42 and is coupled to the actuator piston 44 on the centerline of the actuator 40 within the inner diameter of the springs 52. The position feedback device 58 provides actuator piston position information to a control system (not shown). The centerline coupling reduces the affects of thermal expansion on accuracy and repeatability of the position feedback device 58 over all operating conditions. The position feedback device 58 is an LVDT. In one embodiment, the LVDT is a dual coil, dual rod device (i.e., a duplex device). Alternatively, the LVDT may be a simplex device. The position feedback device 58 may be directly coupled to the actuator piston 44 or may be mounted on bearings that isolate the position feedback device 58.
The valve metering plug 56 is mounted within an aperture 60 of the valve metering plug guide 30. The valve metering plug 56 has a contoured surface 62 that is shaped to provide linear gas flow versus actuator piston stroke (i.e., position) at constant upstream pressure.
The fuel control valve 20 includes a hydraulic filter 64 for last chance filtration of fluid to ensure long lasting operation of the actuator and servo valve 66. The servo valve 66 directs hydraulic fluid to appropriate cavities with the hydraulic manifold 32 to position the actuator piston 44. The servo valve 66 may be simplex, redundant, or a triple coil design.
The valve metering plug guide 30 and hydraulic manifold 32 contain several provisions (i.e. barriers) to maintain fluid to fluid isolation. These barriers protect the hydraulic systems from ingress of high pressure, high temperature gaseous fuels and the gas fuel system from potential ingress from the hydraulic pressure. As previously indicated, the valve metering plug guide 30 acts as a thermal barrier between the valve body 22 and the hydraulic manifold 32. Turning now to FIG. 4, the barriers are provided in a small envelope and consist of leakage paths, vents, and seals. The gas fuel system is protected from the hydraulic system by a pair of hydraulic seals 68 that form a dual redundant seal that reduces leakage of hydraulic fluid from the actuation area 46. Any hydraulic fluid that seeps through the hydraulic seals 68 is routed back into the hydraulic drain connection 70 via a hydraulic leakage path 72. The hydraulic drain connection 70 is shown as being near the fuel inlet for purposes of illustration. Those skilled in the art will recognize that the drain connection 70 may be located anywhere along the hydraulic manifold 32. Hydraulic seal 74 is used to prevent hydraulic fluid from seeping into the gas fuel system. Any hydraulic fluid that seeps past hydraulic seal 74 is vented into the atmosphere via intermediate vent 76.
The hydraulic system is protected from the gas fuel system by a pair of gas seals 78 that form a dual redundant seal that reduces leakage of gaseous fuel from the valve body 22. Any fuel that escapes through the gas seals 78 is routed into a customer vent system via a gas seal leakage path 80. Gas seal 82 is used to prevent gaseous fuel from ingress into the hydraulic system. Any gaseous fuel that flows past gas seal 82 is vented into the atmosphere via intermediate vent 76.
During operation, an external controller commands the servo valve 66 to modulate the position of the actuator piston 44 by directing fluid into or out of the actuation area 46 via paths in the hydraulic manifold 32 to move the actuator piston 44 up or down, thereby moving the valve metering plug 56 to the position required for the desired gaseous fuel flow rate. The output signal of the position feedback device 58 is sent to the external controller for use in the controller's position control loop.
A compact gas fuel control valve has been described. The overall size and weight is approximately fifty percent less than standard commercial valves due to the integration of the actuator 40, hydraulic manifold 32 and valve body 22 into a compact package. The package increases the natural frequency of the control valve 20 to levels that are well above the frequencies that industrial or utility gas turbines operate, which in turn, substantially reduces the susceptibility of failure due to vibration. The elimination of a separate valve bonnet and actuator cylinder cap reduces the number of components in the gas fuel control valve. The reduction of components increases reliability of the system and reduces the cost of the system while maintaining equivalent or greater functionality.
The use of the terms “a” and “an” and “the” and similar referents in the context of describing the invention (especially in the context of the following claims) are to be construed to cover both the singular and the plural, unless otherwise indicated herein or clearly contradicted by context. The use of any and all examples, or exemplary language (e.g., “such as”) provided herein, is intended merely to better illuminate the invention and does not pose a limitation on the scope of the invention unless otherwise claimed. No language in the specification should be construed as indicating any non-claimed element as essential to the practice of the invention.
The foregoing description of various embodiments of the invention has been presented for purposes of illustration and description. It is not intended to be exhaustive or to limit the invention to the precise embodiments disclosed. Numerous modifications or variations are possible in light of the above teachings. The embodiments discussed were chosen and described to provide the best illustration of the principles of the invention and its practical application to thereby enable one of ordinary skill in the art to utilize the invention in various embodiments and with various modifications as are suited to the particular use contemplated. All such modifications and variations are within the scope of the invention as determined by the appended claims when interpreted in accordance with the breadth to which they are fairly, legally, and equitably entitled.

Claims (20)

What is claimed is:
1. A fuel control valve comprising:
a valve body having a fuel inlet, a fuel outlet in fluid communication with the fuel inlet, and a valve metering plug opening;
an actuator piston movably attached to an actuator cylinder having an actuation area;
a hydraulic manifold forming a valve bonnet and an actuator seat, the hydraulic manifold having a hydraulic path in communication with the actuator piston, a hydraulic seal leakage path and a gas seal leakage path, the actuator cylinder connected to the hydraulic manifold at the actuator seat, the hydraulic manifold having a metering plug guide mounted within the valve metering plug opening, the metering plug guide forming a thermal isolation barrier between the valve body and the hydraulic manifold;
a valve metering plug movably mounted within the metering plug guide and directly coupled to the actuator piston, the valve metering plug sealing the fuel outlet from the fuel inlet when at a closed position and providing a variable sized opening to allow fuel to flow at various flow rates when the actuator piston is moved in response to a commanded position; and
wherein the hydraulic seal leakage path is located in the hydraulic manifold between the actuator seat and the thermal isolation barrier and the gas seal leakage path is located between the hydraulic seal leakage path and the valve body.
2. The fuel control valve of claim 1 wherein the hydraulic seal leakage path is routed into a hydraulic drain connection, the fuel control valve further comprising dual redundant hydraulic seals to reduce leakage of hydraulic fluid from the actuation area during operation.
3. The fuel control valve of claim 1 wherein the gas seal leakage path is routed to a vent system, the fuel control valve further comprising dual redundant seals to reduce fuel leakage from the valve body.
4. The fuel control valve of claim 1 wherein the hydraulic manifold includes an intermediate vent routed to atmosphere, the fuel control valve further comprising a seal located between the gas seal leakage path and the intermediate vent.
5. The fuel control valve of claim 4 wherein the hydraulic seal leakage path is routed into a hydraulic drain connection and the gas seal leakage path is routed to a vent system, the fuel control valve further comprising dual redundant hydraulic seals to reduce leakage of hydraulic fluid from the actuation area during operation and dual redundant seals to reduce fuel leakage from the valve body.
6. The fuel control valve of claim 5 wherein the actuator piston has a piston aperture for receiving the valve metering plug.
7. The fuel control valve of claim 6 wherein the valve metering plug is contoured to provide linear gas flow versus actuator piston stroke.
8. The fuel control valve of claim 7 wherein the piston aperture is threaded and the valve metering plug is removably threaded into the piston aperture.
9. The fuel control valve of claim 1 further comprising a position feedback device coupled to the actuator piston on a centerline of the actuator piston.
10. A fuel control valve comprising:
a valve body having a fuel inlet, a fuel outlet in fluid communication with the fuel inlet, and a valve metering plug opening;
an actuator piston having an actuation area, the actuator piston movably attached to an actuator cylinder;
a hydraulic manifold forming a valve bonnet and an actuator seat, the hydraulic manifold having a hydraulic path in fluid communication with the actuation area, the actuator cylinder attached to the hydraulic manifold at the actuator seat, the hydraulic manifold and valve body define an opening that is between the hydraulic manifold and valve body;
a metering plug guide mounted within the valve metering plug opening and the opening and attached to the hydraulic manifold such that fluid in the hydraulic manifold is isolated from high temperature fluid in the valve body to prevent overheating of the fluid in the hydraulic manifold, the metering plug guide having a plug aperture;
a valve metering plug movably mounted within the plug aperture and directly coupled to the actuator piston, the valve metering plug sealing the fuel outlet from the fuel inlet when at a closed position and providing a variable sized opening to allow fuel to flow at various flow rates when the actuator piston is moved in response to a commanded position.
11. The fuel control valve of claim 10 wherein the metering plug guide forms a thermal isolation barrier between the valve body and the hydraulic manifold.
12. The fuel control valve of claim 11 wherein the hydraulic manifold has a hydraulic seal leakage path routed to a hydraulic drain connection and wherein the fuel control valve further comprises as least one hydraulic seal to reduce leakage of hydraulic fluid from the actuation area during operation.
13. The fuel control valve of claim 10 wherein the hydraulic manifold has a gas seal leakage path that is routed to a vent system, the fuel control valve further comprising at least one gas seal to reduce fuel leakage from the valve body.
14. The fuel control valve of claim 13 wherein the hydraulic manifold includes an intermediate vent routed to atmosphere, the fuel control valve further comprising a seal located between the gas seal leakage path and the intermediate vent.
15. The fuel control valve of claim 14 wherein the hydraulic seal leakage path is routed into a hydraulic drain connection and the gas seal leakage path is routed to a vent system, the fuel control valve further comprising dual redundant hydraulic seals to reduce leakage of hydraulic fluid from the actuation area during operation and dual redundant gas seals to reduce fuel leakage from the valve body.
16. The fuel control valve of claim 15 wherein the piston has a threaded piston aperture and the valve metering plug is removably threaded into the threaded piston aperture.
17. The fuel control valve of claim 15 further comprising a position feedback device coupled to the actuator piston on a centerline of the actuator piston.
18. The fuel control valve of claim 17 wherein the position feedback device is an LVDT.
19. A fuel control valve comprising:
a valve body having a fuel inlet, a fuel outlet in fluid communication with the fuel inlet, and a valve metering plug opening;
an actuator piston movably attached to an actuator cylinder having an actuation area;
a hydraulic manifold forming a valve bonnet and an actuator seat, the hydraulic manifold having a hydraulic path in communication with the actuator piston, a hydraulic seal leakage path and a gas seal leakage path, the actuator cylinder connected to the hydraulic manifold at the actuator seat, the hydraulic manifold having a metering plug guide mounted within the valve metering plug opening, the metering plug guide forming a thermal isolation barrier between the valve body and the hydraulic manifold;
a valve metering plug movably mounted within the metering plug guide and directly coupled to the actuator piston, the valve metering plug sealing the fuel outlet from the fuel inlet when at a closed position and providing a variable sized opening to allow fuel to flow at various flow rates when the actuator piston is moved in response to a commanded position;
a position feedback device coupled to the actuator piston on a centerline of the actuator piston; and
wherein the hydraulic seal leakage path is located in the hydraulic manifold between the actuator seat and the thermal isolation barrier and the gas seal leakage path is located between the hydraulic seal leakage path and the valve body.
20. The fuel control valve of claim 19 wherein the hydraulic manifold includes an intermediate vent routed to atmosphere, the hydraulic seal leakage path is routed into a hydraulic drain connection and the gas seal leakage path is routed to a vent system, the fuel control valve further comprising a pair of hydraulic seals to reduce leakage of hydraulic fluid from the actuation area during operation, a pair of gas seals to reduce fuel leakage from the valve body, a gas seal located between the gas seal leakage path and the intermediate vent and a hydraulic seal located between the hydraulic seal leakage path and the intermediate vent.
US09/977,566 2001-10-15 2001-10-15 Control valve with integrated electro-hydraulic actuator Expired - Lifetime US6725876B2 (en)

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AU2002357658A AU2002357658A1 (en) 2001-10-15 2002-10-15 Control valve with integrated electro-hydraulic actuator
PCT/US2002/032860 WO2003033889A2 (en) 2001-10-15 2002-10-15 Control valve with integrated electro-hydraulic actuator
DE10297340T DE10297340B4 (en) 2001-10-15 2002-10-15 Control valve with integrated electrohydraulic actuator
JP2003536596A JP4272062B2 (en) 2001-10-15 2002-10-15 Control valve with integrated electrohydrodynamic actuator

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Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20070102049A1 (en) * 2005-11-09 2007-05-10 Honeywell International, Inc. Valve actuator assembly
US20090020165A1 (en) * 2007-07-17 2009-01-22 Wolfgang Oelerich Fuel leakage vent for fuel source and valve interface
US20100043760A1 (en) * 2008-08-21 2010-02-25 Cummins Inc. Fuel pump
US20100170583A1 (en) * 2009-01-06 2010-07-08 Woodward Governor Company Fluid Control Valve
CN101705871B (en) * 2009-11-20 2012-05-09 株洲南方燃气轮机成套制造安装有限公司 Gas fuel regulating valve of combustion gas turbine
US20130167950A1 (en) * 2010-08-06 2013-07-04 Kawasaki Jukogyo Kabushiki Kaisha Gas pressure regulating valve
US20130340609A1 (en) * 2011-03-10 2013-12-26 Waters Technologies Corporation Pump head outlet port
RU2589413C2 (en) * 2011-03-16 2016-07-10 Сименс Акциенгезелльшафт Speed transmitter for gas turbine
US9644646B2 (en) * 2011-02-18 2017-05-09 Norgren, Inc. Multiple-staged fluid operated actuator
US20170130868A1 (en) * 2015-11-05 2017-05-11 Fisher Controls International Llc Balanced valve trim and method of reducing stem forces on a valve stem
US9926803B2 (en) 2016-06-28 2018-03-27 Woodward, Inc. Turbine control device prognostics
US10302205B2 (en) * 2017-07-04 2019-05-28 Hawe Hydraulik Se Hydraulic component with a valve unit and hydraulic system with a hydraulic component

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8534323B2 (en) * 2009-04-10 2013-09-17 Flowserve Corporation Control valves and methods of flowing a material through a control valve
US9869403B2 (en) * 2011-05-09 2018-01-16 Hamilton Sundstrand Corporation Valve having pressure-relieving vent passage
US20170051676A1 (en) * 2014-04-28 2017-02-23 Moog Inc. Turbine combustion chamber pressure assisted control valve
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US11873921B2 (en) * 2021-08-10 2024-01-16 Electric Power Research Institute, Inc. Servo-controlled metering valve and fluid injection system

Citations (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3051432A (en) * 1960-02-18 1962-08-28 Sullivan Valve & Engineering Co Two-stage hydromotor-operated valve
US3112876A (en) * 1960-08-25 1963-12-03 Sullivan Valve & Engineering Co Two-stage valve having floating switches
US3307574A (en) * 1964-02-07 1967-03-07 Acf Ind Inc Drain structure for venting leaked fluid from valve stem packing
US3379405A (en) * 1966-01-03 1968-04-23 Acf Ind Inc Valve
US3427930A (en) * 1965-07-02 1969-02-18 Fisher Governor Co Valve actuator
US3563508A (en) * 1968-12-13 1971-02-16 Bruce L Delorenzo Valve including piston with spaced apart plates
DE2047975A1 (en) * 1969-10-02 1971-07-15 Nakakita Seisakusho Procedure for automatic valve control
US4311296A (en) * 1978-08-16 1982-01-19 Gerd Scheffel Cartridge element control
US4340086A (en) * 1979-04-19 1982-07-20 Sperry Vickers, Division Of Sperry Gmbh Hydraulic control valve unit
US4478245A (en) * 1981-09-02 1984-10-23 Vickers, Incorporated Electrically controllable valve assembly
US4724864A (en) * 1984-12-21 1988-02-16 Hans Schwelm Two-way flow control valve
EP0286722A1 (en) * 1987-04-11 1988-10-19 VDO Mess- und Regeltechnik GmbH Electropneumatic position controller
US4865074A (en) * 1988-06-20 1989-09-12 Keystone International Inc. High temperature safety relief system
US4872639A (en) * 1987-08-25 1989-10-10 Societe D'exploitation De Brevets Pour L'industrie Et La Marine Sebim Pilot-control safety valve
US5074519A (en) * 1990-11-09 1991-12-24 Cooper Industries, Inc. Fail-close hydraulically actuated control choke
US5172719A (en) * 1991-07-19 1992-12-22 Westinghouse Electric Corp. Steam turbine control valve
US5203370A (en) * 1991-11-26 1993-04-20 Block Gary C Mounting apparatus with fugitive emission collection means for directly coupling a rotary valve to an actuator having rotary drive means
US5251148A (en) * 1990-06-01 1993-10-05 Valtek, Inc. Integrated process control valve
US5445188A (en) * 1993-05-27 1995-08-29 Hydrolux S.A.R.L. Pilot operated servo valve
US5549137A (en) * 1993-08-25 1996-08-27 Rosemount Inc. Valve positioner with pressure feedback, dynamic correction and diagnostics
US5896890A (en) * 1994-11-06 1999-04-27 Hydrolux S.A R.L. Pilot-operated servo-valve
US6056008A (en) * 1997-09-22 2000-05-02 Fisher Controls International, Inc. Intelligent pressure regulator
US6267349B1 (en) * 1992-09-25 2001-07-31 Target Rock Corporation Precision valve control

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3427830A (en) * 1967-05-03 1969-02-18 Z Textilniho Strojirenstvi Gen Drive arrangement for oscillating the needle cylinder of a circular knitting machine

Patent Citations (25)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3051432A (en) * 1960-02-18 1962-08-28 Sullivan Valve & Engineering Co Two-stage hydromotor-operated valve
US3112876A (en) * 1960-08-25 1963-12-03 Sullivan Valve & Engineering Co Two-stage valve having floating switches
US3307574A (en) * 1964-02-07 1967-03-07 Acf Ind Inc Drain structure for venting leaked fluid from valve stem packing
US3427930A (en) * 1965-07-02 1969-02-18 Fisher Governor Co Valve actuator
US3379405A (en) * 1966-01-03 1968-04-23 Acf Ind Inc Valve
US3563508A (en) * 1968-12-13 1971-02-16 Bruce L Delorenzo Valve including piston with spaced apart plates
DE2047975A1 (en) * 1969-10-02 1971-07-15 Nakakita Seisakusho Procedure for automatic valve control
US4311296A (en) * 1978-08-16 1982-01-19 Gerd Scheffel Cartridge element control
US4340086A (en) * 1979-04-19 1982-07-20 Sperry Vickers, Division Of Sperry Gmbh Hydraulic control valve unit
US4478245A (en) * 1981-09-02 1984-10-23 Vickers, Incorporated Electrically controllable valve assembly
US4724864A (en) * 1984-12-21 1988-02-16 Hans Schwelm Two-way flow control valve
EP0286722A1 (en) * 1987-04-11 1988-10-19 VDO Mess- und Regeltechnik GmbH Electropneumatic position controller
US4872639A (en) * 1987-08-25 1989-10-10 Societe D'exploitation De Brevets Pour L'industrie Et La Marine Sebim Pilot-control safety valve
US4865074A (en) * 1988-06-20 1989-09-12 Keystone International Inc. High temperature safety relief system
US5251148A (en) * 1990-06-01 1993-10-05 Valtek, Inc. Integrated process control valve
US5074519A (en) * 1990-11-09 1991-12-24 Cooper Industries, Inc. Fail-close hydraulically actuated control choke
US5172719A (en) * 1991-07-19 1992-12-22 Westinghouse Electric Corp. Steam turbine control valve
US5203370A (en) * 1991-11-26 1993-04-20 Block Gary C Mounting apparatus with fugitive emission collection means for directly coupling a rotary valve to an actuator having rotary drive means
US6267349B1 (en) * 1992-09-25 2001-07-31 Target Rock Corporation Precision valve control
US5445188A (en) * 1993-05-27 1995-08-29 Hydrolux S.A.R.L. Pilot operated servo valve
US5549137A (en) * 1993-08-25 1996-08-27 Rosemount Inc. Valve positioner with pressure feedback, dynamic correction and diagnostics
US5573032A (en) * 1993-08-25 1996-11-12 Rosemount Inc. Valve positioner with pressure feedback, dynamic correction and diagnostics
US5896890A (en) * 1994-11-06 1999-04-27 Hydrolux S.A R.L. Pilot-operated servo-valve
US6056008A (en) * 1997-09-22 2000-05-02 Fisher Controls International, Inc. Intelligent pressure regulator
US6178997B1 (en) * 1997-09-22 2001-01-30 Fisher Controls International, Inc. Intelligent pressure regulator

Non-Patent Citations (6)

* Cited by examiner, † Cited by third party
Title
Declaration of Jeff Stewart-4 pages.
Declaration of Jeff Stewart—4 pages.
Information Disclosure Statement pursuant to 37 CFR § 1.56-3 pages.
Information Disclosure Statement pursuant to 37 CFR § 1.56—3 pages.
Stewart Affidavit-1 page.
Stewart Affidavit—1 page.

Cited By (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7537022B2 (en) 2005-11-09 2009-05-26 Honeywell International Inc. Valve actuator assembly
US20070102049A1 (en) * 2005-11-09 2007-05-10 Honeywell International, Inc. Valve actuator assembly
US20090020165A1 (en) * 2007-07-17 2009-01-22 Wolfgang Oelerich Fuel leakage vent for fuel source and valve interface
US7896023B2 (en) * 2007-07-17 2011-03-01 GM Global Technology Operations LLC Fuel leakage vent for fuel source and valve interface
US9151289B2 (en) * 2008-08-21 2015-10-06 Cummins Inc. Fuel pump
US20100043760A1 (en) * 2008-08-21 2010-02-25 Cummins Inc. Fuel pump
US20100170583A1 (en) * 2009-01-06 2010-07-08 Woodward Governor Company Fluid Control Valve
US8038121B2 (en) 2009-01-06 2011-10-18 Woodward, Inc. Fluid control valve with sensing port
CN101705871B (en) * 2009-11-20 2012-05-09 株洲南方燃气轮机成套制造安装有限公司 Gas fuel regulating valve of combustion gas turbine
US20130167950A1 (en) * 2010-08-06 2013-07-04 Kawasaki Jukogyo Kabushiki Kaisha Gas pressure regulating valve
US8960221B2 (en) * 2010-08-06 2015-02-24 Kawasaki Jukogyo Kabushiki Kaisha Gas pressure regulating valve
US9644646B2 (en) * 2011-02-18 2017-05-09 Norgren, Inc. Multiple-staged fluid operated actuator
US20130340609A1 (en) * 2011-03-10 2013-12-26 Waters Technologies Corporation Pump head outlet port
RU2589413C2 (en) * 2011-03-16 2016-07-10 Сименс Акциенгезелльшафт Speed transmitter for gas turbine
US10156191B2 (en) 2011-03-16 2018-12-18 Siemens Aktiengesellschaft Stroke transmitter for gas turbine
US20170130868A1 (en) * 2015-11-05 2017-05-11 Fisher Controls International Llc Balanced valve trim and method of reducing stem forces on a valve stem
US10094488B2 (en) * 2015-11-05 2018-10-09 Fisher Controls International Llc Balanced valve trim and method of reducing stem forces on a valve stem
US9926803B2 (en) 2016-06-28 2018-03-27 Woodward, Inc. Turbine control device prognostics
US10302205B2 (en) * 2017-07-04 2019-05-28 Hawe Hydraulik Se Hydraulic component with a valve unit and hydraulic system with a hydraulic component

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JP2005506496A (en) 2005-03-03
DE10297340B4 (en) 2011-02-17
JP4272062B2 (en) 2009-06-03
WO2003033889A2 (en) 2003-04-24
WO2003033889A3 (en) 2003-05-30
DE10297340T5 (en) 2004-11-11
US20030070711A1 (en) 2003-04-17
AU2002357658A1 (en) 2003-04-28

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